US3595590A - Piston ring - Google Patents
Piston ring Download PDFInfo
- Publication number
- US3595590A US3595590A US835645A US3595590DA US3595590A US 3595590 A US3595590 A US 3595590A US 835645 A US835645 A US 835645A US 3595590D A US3595590D A US 3595590DA US 3595590 A US3595590 A US 3595590A
- Authority
- US
- United States
- Prior art keywords
- layer
- wear
- piston ring
- sliding
- resistant
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 24
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 21
- 239000011651 chromium Substances 0.000 claims abstract description 20
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims abstract description 19
- 239000011733 molybdenum Substances 0.000 claims abstract description 19
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 16
- 239000000463 material Substances 0.000 claims description 33
- 230000000994 depressogenic effect Effects 0.000 claims description 10
- 239000011248 coating agent Substances 0.000 claims description 7
- 238000000576 coating method Methods 0.000 claims description 7
- 238000000227 grinding Methods 0.000 abstract description 7
- 238000007747 plating Methods 0.000 description 6
- 239000000203 mixture Substances 0.000 description 4
- 229910001018 Cast iron Inorganic materials 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000005488 sandblasting Methods 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 1
- 238000003486 chemical etching Methods 0.000 description 1
- 239000010431 corundum Substances 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 238000010285 flame spraying Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 238000007788 roughening Methods 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 239000011573 trace mineral Substances 0.000 description 1
- 235000013619 trace mineral Nutrition 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/26—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction characterised by the use of particular materials
Definitions
- the present invention relates to a piston ring whose cylinder-contacting surface has axially arranged bands of a wear resistant material such as chromium and a sliding-friction resistant material such as molybdenum.
- Molybdenum surfaces on piston rings have less tendency than other surfaces to develop pitting. However, molybdenum surfaces are not as resistant to wear as are surfaces of, for example, hard chromium.
- Piston rings having an insert ring on which a chromium surface has been applied are already known. Furthermore, at-
- run-in surfaces have been imbedded in one or more grooves on the chrome-plated surface of a piston ring. Such grooves have extended through to the basic piston ring material, so that a strong bonding of the runin material to the base material was achieved. It is also known to make the run-in surface of molybdenum or titanium andto extend such material axially so that it entirely covers the chromium layer. However, then the different materials are not utilized at the same time but only one after the other.
- piston rings with edge bands of chromium or molybdenum and having a central band of the basic material of the ring are known.
- the central band may be convex, concave, or planar.
- FIG. I is a section of a piston ring according to the invention, the section plane including the axis of the ring.
- FIG. 2 is a section as in FIG. I of a second piston ring according to the invention. 7
- FIG. 3 is a section as in FIG. I of a third piston ring according to the invention.
- FIG. 4 is a section through grinding apparatus, the section plane being perpendicular to the rotation axes.
- FIG. is a partially schematic, partially sectional elevation of an electroplating apparatus.
- FIG. 6 is a schematic illustration of a flame-spraying process.
- FIG. 7 is a section as in FIG. 1 of the piston ring of FIG. I before its manufacture is complete.
- the support ring 1 of the piston ring of FIG. I has a central protrusion 2 projecting radially relative to piston ring axis 20 outwards on its outer surface 13, thus creating depressions 35 of constant and equal radius R,,,.
- a substantially uniformly thick layer 3 of hard chromium, a wear-resistant material is provided on this outer surface.
- the depressed portions of the hard chrome have been built up with layers 4 and 5 of molybdenum, a sliding-friction resistant material.
- the support ring 6 of FIG. 2 exhibits a radial protrusion 7 at its lower edge.
- the outer surface of this support ring has been coated with a layer 8 if chromium of substantially uniform thickness, and the depressed region of the chrome layer adjoining that on protrusion 7 is provided with a layer 9 of molybdenum.
- the support ring 10 has a wave-shaped profile with three protrusions on its outer surface.
- the resulting depressions in the hard-chrome layer 11 are filled with molybdenum layers 12.
- the difference R R, in FIG. 1 equals l.5 mm.
- composition of the cast iron of the support ring is as follows:
- the cast iron support ring 1 is then prepared for plating on its outer surface 13 by turning.
- the support ring I is then clamped between plastic plates 28 by bolt and wing nut'29. Rubber washers 30 are provided to seal the interior of the ring from the plating solution 31, whose composition is 250 g/l Cro,
- switch 34 Upon hanging the assembly in the plating solution using rod 32 and hooks 33, switch 34 is closed for about 5 hours, during which time the current density at the outer surface 13 is 50 Amp./dm.
- the anode is made of lead. This places a hard chrome layer 3 of thickness 0.2 mm. on the outer surface 13.
- the hard chrome surface is roughened by sand blasting using as sand corundum, silicon carbide, or diamond dust.
- the support ring is then ready for application of Mo, as a sliding-friction resistant material, in the depressions 35 of the hard chrome surface.
- the toughening enables a better bonding of the Mo and provides oil catching pockets in any finally exposed chromium.
- a preferred surface roughness is circa 20 Rt.
- FIG. 6 shows the chrome-plated support ring I mounted for rotation with spindle 36.
- Spindle 36 is mounted at its ends in any conventional means to effect its rotation.
- the tangential surface velocity v, of the support ring 1 is 50 meters per minute.
- the thickness t of the support ring is 4.5 mm.
- the flame spray gun 37 is fed by a molybdenum supply 38 and a fuel and compressed gas supply 39.
- the nozzle cone angle of the gun 37 and its distance from the surface of the support ring 1 are chosen to maximize uniformity of deposition while minimizing losses due to missing of the ring and subsequently required finish grinding. Such considerations are well known in the art.
- the flame spray gun 37 blows atomized molten molybdenum onto the chrome surface of the support ring 1.
- the composition of the fuel is a mixture of acetylene and oxygen in such proportions that the flame is nearly neutral, i.e., neither oxydizing nor reducing. It is burned with oxygen as oxidant at zero percent by weight excess oxygen.
- the entire surface of molybdenum is applied in six passes of the support ring.
- the molybdenum is allowed to build up an excess thickness e (FIG. 7) of about 0.2 mm. over the chromium on the protrusion 2, in order that depressions 35 become completely filled.
- This extra thickness is subsequently removed to yield the finished piston ring of FIG. 1 by a grinding operation similar to that depicted in FIG. 4. This final grinding assures that at the abutment between the exposed faces of Cr and M the exposed-face radius is continuous in passing from the Mo face to the Cr face or vice versa, as opposed to a discontinuous behavior which would be present ifa ledge existed at the abutment.
- the exposed-face radius R is a constant in FIG. I, while it varies as a function of axial distance in FIG. 2, the variation of R, in FIG. 2 at the Mo-Cr abutment nevertheless being continuous.
- the spraying of FIG. 6 is carried out in an atmosphere of air.
- the hard-chrome layer can be replaced by a hardnickel layer, and the surface of wear-resistant material can be roughened by a chemical etching process before application of the sliding-friction resistant surface, instead of using a sand blasting operation.
- a piston ring comprising a support ring having an outer surface provided with a radial protrusion whereby part of the outer surface is radially depressed relative to said protrusion, a layer of wear-resistant material coating the outer surface of said support ring, said layer of wear-resistant material having a substantially uniform thickness whereby its outer surface is a replica of the outer surface of said support ring, and a layer of sliding-friction resistant material coating said layer of wear-resistant material in its radially depressed part.
- a piston ring as claimed in claim 1 said protrusion being centrally located in the outer surface of said support ring, the depressed part of the outer surface being of constant equal radius.
- a piston ring as claimed in claim 1 the depressed part of the outer surface being of constant and equal radius, said layers of wear-resistant material and sliding-friction resistant material having exposed faces of constant radius.
- a piston ring as claimed in claim 1 said sliding-friction resistant material coating said layer of wear-resistant material on a roughened face thereof.
- a piston ring as claimed in claim 1 said wear-resistant and sliding-friction resistant layers having exposed faces, the exposed-face radius being continuous in passing from the wear-resistant layer to the sliding-friction resistant layer or vice versa.
- a piston ring as claimed in claim 8 said wear-resistant layer being chromium.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Coating By Spraying Or Casting (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19681751573 DE1751573C3 (de) | 1968-06-21 | Kolbenring für Brennkraftmaschinen |
Publications (1)
Publication Number | Publication Date |
---|---|
US3595590A true US3595590A (en) | 1971-07-27 |
Family
ID=5692359
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US835645A Expired - Lifetime US3595590A (en) | 1968-06-21 | 1969-06-23 | Piston ring |
Country Status (3)
Country | Link |
---|---|
US (1) | US3595590A (de) |
FR (1) | FR2011353A1 (de) |
GB (1) | GB1269704A (de) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3762010A (en) * | 1969-08-15 | 1973-10-02 | Nippon Piston Ring Co Ltd | Piston ring and manufacture thereof |
JPS50158751A (de) * | 1974-06-14 | 1975-12-22 | ||
US4176434A (en) * | 1977-01-19 | 1979-12-04 | Koppers Company, Inc. | Method of making piston rings with chrome-filled grooves |
US6325385B1 (en) * | 1998-10-15 | 2001-12-04 | Teikoku Piston Ring Co., Ltd. | Piston ring |
US20100044967A1 (en) * | 2007-02-17 | 2010-02-25 | Johannes Esser | Piston ring |
EP3530400A1 (de) * | 2018-02-23 | 2019-08-28 | MAN Truck & Bus SE | Verfahren zum herstellen eines bauteils, insbesondere fahrzeugbauteils, und entsprechend hergestelltes bauteil |
US11365806B2 (en) | 2019-09-09 | 2022-06-21 | Tenneco Inc. | Coated piston ring for an internal combustion engine |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5412022A (en) * | 1977-06-25 | 1979-01-29 | Goetzewerke | Machine portion material exposed to wear that has coating layer on sliding surface in shape that riser portion is mounted to one side or both sides |
-
1969
- 1969-02-26 FR FR6904925A patent/FR2011353A1/fr not_active Withdrawn
- 1969-06-20 GB GB31403/69A patent/GB1269704A/en not_active Expired
- 1969-06-23 US US835645A patent/US3595590A/en not_active Expired - Lifetime
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3762010A (en) * | 1969-08-15 | 1973-10-02 | Nippon Piston Ring Co Ltd | Piston ring and manufacture thereof |
JPS50158751A (de) * | 1974-06-14 | 1975-12-22 | ||
US4176434A (en) * | 1977-01-19 | 1979-12-04 | Koppers Company, Inc. | Method of making piston rings with chrome-filled grooves |
US6325385B1 (en) * | 1998-10-15 | 2001-12-04 | Teikoku Piston Ring Co., Ltd. | Piston ring |
US20100044967A1 (en) * | 2007-02-17 | 2010-02-25 | Johannes Esser | Piston ring |
US8356820B2 (en) * | 2007-02-17 | 2013-01-22 | Federal-Mogul Burscheid Gmbh | Piston ring |
EP3530400A1 (de) * | 2018-02-23 | 2019-08-28 | MAN Truck & Bus SE | Verfahren zum herstellen eines bauteils, insbesondere fahrzeugbauteils, und entsprechend hergestelltes bauteil |
CN110185550A (zh) * | 2018-02-23 | 2019-08-30 | 曼卡车和巴士股份公司 | 用于制造构件特别是车辆构件的方法和相应地制造的构件 |
US11498126B2 (en) | 2018-02-23 | 2022-11-15 | Man Truck & Bus Ag | Method for producing a component, in particular vehicle component, and correspondingly produced component |
US11365806B2 (en) | 2019-09-09 | 2022-06-21 | Tenneco Inc. | Coated piston ring for an internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
FR2011353A1 (de) | 1970-02-27 |
DE1751573A1 (de) | 1971-05-19 |
DE1751573B2 (de) | 1977-05-18 |
GB1269704A (en) | 1972-04-06 |
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